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  • DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT

    Available format(s):  Hardcopy, PDF

    Superseded date:  19-09-2016

    Language(s):  English

    Published date:  01-01-2015

    Publisher:  UK Ministry of Defence Standards

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    Table of Contents - (Show below) - (Hide below)

    Preface
    SECTION 6 - EQUIPMENT
    SUPPLEMENTS

    Abstract - (Show below) - (Hide below)

    Describes the requirements relating to equipment and systems embodied on any aircraft.

    General Product Information - (Show below) - (Hide below)

    Development Note Supersedes DEFSTAN 00-970(PT1)SEC6/14(2015). (09/2015)
    Document Type Standard
    Publisher UK Ministry of Defence Standards
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    BS 3J 12:1991 Specification for pressure-sensitive adhesive identification tape
    BS C 18:1976 Specification for V-flange couplings for aircraft piping and ducting - metric series
    DEFSTAN 00-35(PT4)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 4: NATURAL ENVIRONMENTS
    BS G 230:1984 Specification for general requirements for aircraft electrical cables (second series)
    BS 2G 143:1965 Specification for a.c. and d.c. rotary and linear actuators for aircraft
    BS 2G 180:1974 Specification for permanent splicing of aircraft electrical cables
    DEFSTAN 00-13/3(1994) : 1994 REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT
    BS 2G 134:1970 Specification for d.c. generators
    BS 2G 210:1991 Specification for PTFE insulated equipment wires and cables, single and multi-core, with silver plated copper conductors (190°C) or nickel plated copper conductors (260°C)
    BS M 43:1973 Methods of zoning aircraft and referencing access doors and panels
    DEFSTAN 81-24/5(2004) : 2004 IDENTIFICATION MARKING OF TRANSPORTABLE CONTAINERS, COMPRESSED GAS
    BS M 55:1984 Method for rotary flexure testing of hydraulic tubing joints and fittings for aerospace use
    DEFSTAN 00-35(PT5)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS
    BS 5M 23:1987 Specification for an identification scheme for pipelines
    BS M 51:1982 Classification for pressure and temperature for fluid systems and components
    DEFSTAN 59-97/3(1990) : AMD 1 HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL
    DEFSTAN 05-42/2(1982) : 1982 PARTICULATE CONTAMINATION CLASSES FOR FLUIDS IN HYDRAULIC SYSTEMS
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    BS G 231:1983 Specification for conductors for general purpose aircraft electrical cables and aerospace applications
    BS G 207:1969 Specification for aircraft electrical circuit diagrams
    BS 3G 197:1982 Specification for stud-type terminal blocks for terminations on aircraft electric cables
    MIL A 5498 : D ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT
    DEFSTAN 01-5/17(2011) : 2011 FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS
    ISO 6771:2007 Aerospace Fluid systems and components Pressure and temperature classifications
    DEFSTAN 00-35(PT1)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 1: CONTROL AND MANAGEMENT
    DEFSTAN 05-43/1(1977) : 1977 STANDARD PROCEDURES FOR TAKING SAMPLES OF HYDRAULIC FLUIDS FOR EVALUATION OF PARTICULATE CONTAMINATION
    DEFSTAN 61-12(PT9)/5(2008) : 2008 WIRES, CORDS AND CABLES ELECTRICAL - METRIC UNITS - PART 9: CABLES AND WIRES ELECTRICAL FOR CABLES, RADIO FREQUENCY INCLUDING LIMITED FIRE HAZARD (LFH) VARIANTS
    MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
    BS M 52:1983 Method for impulse testing of hydraulic hose, tubing and fittings assemblies for aerospace fluid systems
    BS 2G 202:1988 Specification for design and performance requirements for airframe-fit electrical connectors for d.c. and low frequency a.c. applications
    DEFSTAN 59-35(PT0)/3(1990) : 1990 CONNECTORS ELECTRICAL - PART 0: GUIDE TO CONNECTORS ELECTRICAL, DIRECT CURRENT, LOW FREQUENCY AND RADIO FREQUENCY APPLICATIONS
    BS G 212:1971 Specification for general requirements for aircraft electrical cables
    MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
    BS 2G 127:1967 Specification for power and current transformers for use in aircraft electrical power supply systems
    BS 2G 100-2:1962 Specification for general requirements for electrical equipment and indicating instruments for aircraft Environmental and operating conditions
    ISO 6772:2012 Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies
    BS M 53:1983 Method for thermal shock testing of pipes and fittings for aerospace fluid systems
    STANAG 3323 : 0 PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC)
    DEFSTAN 00-31/1(1987) : 1987 THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS
    BS M 44:1974 Specification for identification of aircraft servicing, maintenance, ground handling and safety/hazard points
    ISO 7169:2014 Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric
    DEFSTAN 00-971/1(1987) : 1987 GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES
    DOD STD 1788 : LATEST AVIONICS INTERFACE DESIGN STANDARD (METRIC)
    BS G 209:1970 Specification for transformer rectifier units
    BS 2G 232:1987 Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation
    DEFSTAN 00-35(PT3)/4(2006) : 2006 ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS
    MIL-PRF-5503 Revision G:2013 ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR
    BS M 48:1975 Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series
    BS 5G 205-1:1990 Secondary batteries for aircraft Specification for lead-acid batteries
    BS M 60:1986 Specification for separable tube fittings for fluid systems
    BS 2G 146:1966 Specification for d.c. motors for aircraft
    BS G 203:1967 Specification for Unified screws with captive facing and locking washers
    BS 2G 223:1989 Specification for screen terminating devices for aircraft electric cables
    BS 2G 229:1987 Schedule for environmental conditions and test procedures for airborne equipment
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    BS 2G 199:1984 Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration
    BS 6275-1:1982 Hydraulic fluid power filter elements Method of evaluating filtration performance (multi-pass method)
    BS C 13:1960 Sizes of gravity filling orifices on aircraft
    DEFSTAN 61-10/4(1984) : 1984 GENERATOR SETS (GROUND, ENGINE DRIVEN)
    MIL-D-81641 Base Document:1972 DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR
    DEFSTAN 00-41(PT1)/2(1989) : 1989 MOD PRACTICES AND PROCEDURES FOR RELIABILITY AND MAINTAINABILITY - PART 1: RELIABILITY DESIGN PHILOSOPHY
    MIL-H-8775 Revision D:1976 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
    BS 2G 196:1971 Specification for static invertors
    MIL D 87213 : 0 DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
    ISO 7257:2016 Aircraft Hydraulic tubing joints and fittings Rotary flexure test
    BS 2G 219:1983 Specification for general requirements for ground support electrical supplies for aircraft
    BS C 9:1970 Specification for coupling dimensions for high pressure air charging valves for aircraft
    MIL F 8815 : D FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR
    MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
    BS 2G 100-3:1968 General requirements for aircraft electrical equipment and indicating in struments Characteristics of aircraft electrical systems
    BS G 217:1975 Specification for general requirements for cockpit lighting controllers
    ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING
    BS G 194:1965 Specification for lever-operated manual switches for aircraft
    BS 3G 233:1990 Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation
    BS G 102:1971 Specification for general requirements for rotating electrical machinery
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    BS 4G 229:1996 Schedule for environmental conditions and test procedures for airborne equipment
    MIL-I-8700 Revision A:1970 INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR
    BS G 222:1976 Specification for Efglas type electric cables (metric units)
    DEFSTAN 00-970/VOL1/1(1983) : AMD 14 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES
    DEFSTAN 00-970/VOL2/1(1984) : 1984 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT
    STANAG 3212 : 2017 DIAMETERS FOR GRAVITY FILLING ORIFICES
    DEFSTAN 00-52/4(2014) : 2014 THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES
    ISO 6773:1994 Aerospace Fluid systems Thermal shock testing of piping and fittings
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